Ram air intakes of rotary-wing aircraft turbine engines

Details Ram air intakes of rotary-wing aircraft turbine engines Ram air intakes of rotary-wing aircraft turbine engines

1974-11-07

1976-12-21

Croyle, Carlton R.

Power plants

Combustion products used as motive fluid

With safety device

55306, F02C 704

Patent

active

039980480

ABSTRACT:
The invention relates to equipment for the air intake of an aircraft turbine engine, which equipment includes an inlet duct capable of being obturated by a bullet therein, and a bullet thrust mechanism connected to the duct by studs forming bullet guides. Part of the duct is formed by box members for receiving a plurality of separating elements downstream of deflectors, the internal face of the duct lip together with the external face of the bullet and of a jack piston and cylinder of said thrust mechanism being made of soundproofing material.

REFERENCES:
patent: 3082792 (1963-03-01), Jenkins
patent: 3302396 (1967-02-01), Robbins
patent: 3421246 (1969-01-01), Beurer
patent: 3483676 (1969-12-01), Sangisson
patent: 3508838 (1970-04-01), Martenson
patent: 3692141 (1972-09-01), Labussiene
patent: 3811254 (1974-05-01), Amelio

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